diff --git a/+af_tools/@Polar/Polar.m b/+af_tools/@Polar/Polar.m
index 69fbc62174ccb2da4668d25048bc98d86d3b849d..524377a009195f817daaf2be28d254e93ec1e4ee 100644
--- a/+af_tools/@Polar/Polar.m
+++ b/+af_tools/@Polar/Polar.m
@@ -181,7 +181,7 @@ classdef Polar < handle
         self = polypolar(polyCl, polyCd) % Create polar using polynomial coefficients
 
         % Create a polar by interpolating between two different polar objects
-        self = interppolar(Polar1, Polar2, position)
+        self = interppolar(Polar1, Polar2, weightPolar2)
     end
 
 end
diff --git a/+af_tools/@Polar/interppolar.m b/+af_tools/@Polar/interppolar.m
index 054ff051bdb04b7375390b3ed01511f95281be13..3b8d661f68fdc8ee70bd179e4fac68e201eed4dc 100644
--- a/+af_tools/@Polar/interppolar.m
+++ b/+af_tools/@Polar/interppolar.m
@@ -1,6 +1,6 @@
 function self = interppolar(Polar1, Polar2, weightPolar2)
     % INTERPPOLAR  Create a new polar object by interpolation of two other polars.
-    %   This static method can be used in place of a normal constructor.
+    %   This static method can be used in place of a normal constructor for the Polar class.
     %   This method can be used when the user wants to interpolate the polars bewteen two known
     %   airfoils. Consider that the airfoil at x=0 is a NACA 0012, and the one at x=1 is a CLARY-Y.
     %   Rather than assuming that all segments in [0,1] are NACA 0012 and all segments after 1 are
@@ -8,7 +8,7 @@ function self = interppolar(Polar1, Polar2, weightPolar2)
     %   the two bounds. If we are at 0.1, the newly created Polar object, will then be 90% of NACA
     %   0012 and 10% of CLARK-Y.
     % Note:
-    %   The two input Polars should have the same range of AOA, Reynolds, Mach, and nCrit.
+    %   The two input Polars should have the same range of Reynolds, Mach, and nCrit.
     % -----
     %
     % Usage:
@@ -27,7 +27,7 @@ function self = interppolar(Polar1, Polar2, weightPolar2)
     % Example:
     %   MixedPolar = af_tools.interppolar(PolarNACA0012, PolarClarkY, 0.6); Creates an interpolated
     %                Polar object MixedPolar that results from the interpolation of PolarNACA0012
-    %                and PolarClarkY, asusming that the MixedPolar is made of 60% ClarkY and 40%
+    %                and PolarClarkY, assuming that the MixedPolar is made of 60% ClarkY and 40%
     %                NACA0012.
     %
     % See also: af_tools.Polar.
@@ -45,7 +45,7 @@ function self = interppolar(Polar1, Polar2, weightPolar2)
     % ----------------------------------------------------------------------------------------------
 
     % --- Defaults and constants
-    DEBUG = true;
+    DEBUG = false;
 
     % --- Input checks
     % Check if both Polars are Polars objects and weightPolar2 is in [0,1]
@@ -54,8 +54,7 @@ function self = interppolar(Polar1, Polar2, weightPolar2)
     validateattributes(weightPolar2, {'double'}, {'scalar', 'nonnegative', '<=', 1}, ...
                        mfilename(), 'weightPolar2', 3);
 
-    % Check that both Polars have the same AOA, Reynolds, Mach and nCrit
-    equalfieldscheck(Polar1, Polar2, 'aoa');
+    % Check that both Polars have the Reynolds, Mach and nCrit
     equalfieldscheck(Polar1, Polar2, 'reynolds');
     equalfieldscheck(Polar1, Polar2, 'mach');
     equalfieldscheck(Polar1, Polar2, 'nCrit');
@@ -64,6 +63,25 @@ function self = interppolar(Polar1, Polar2, weightPolar2)
 
     self = af_tools.Polar;
 
+    if Polar1 == Polar2
+        self.properties = self.properties;
+        self.airfoil = self.airfoil;
+        self.reynolds = self.reynolds;
+        self.mach = self.mach;
+        self.nCrit = self.nCrit;
+        self.aoa  = self.aoa;
+        self.cl   = self. cl;
+        self.cd  = self.cd;
+        self.cm = self.cm;
+
+        self.Ext = self.Ext;
+        self.Stall = self.Stall;
+        self.Zero = self.Zero;
+        self.Lin = self.Lin;
+        self.extrapMethod = self.extrapMethod;
+        return
+    end
+
     wPol2 = weightPolar2;
     wPol1 = 1 - wPol2;
     nPolars = numel(Polar1.reynolds);
@@ -118,8 +136,10 @@ function self = interppolar(Polar1, Polar2, weightPolar2)
             plot(Polar1.aoa(:, j), Polar1.cl(:, j));
             plot(Polar2.aoa(:, j), Polar2.cl(:, j));
             plot(self.aoa(:, j), self.cl(:, j));
+            hold off;
             legend(Polar1.airfoil{1}, Polar2.airfoil{1}, self.airfoil{1}, 'Location', 'NorthWest');
             grid on;
+            pause;
         end
     end